Numerical study on stability of oblique wing configuration

Syed Mohamed Ali, Jaffar and M.Shaari, Muhammad Hafiz (2023) Numerical study on stability of oblique wing configuration. In: IIUM Engineering Congress, 15-16 August 2023, KOE ,IIUM.

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Abstract

Oblique wing is one of the morphing wing configurations that offer a superior high speed aerodynamic performance. The mechanism in which a straight wing is being rotated by a pivot at the centre resulting swept back wing on one side and swept forward on the other side. It was proven that this configuration was able to reduce drag for a given lift at both supersonic cruise and subsonic; however, there are serious control issues. CFD analysis using SolidWorks software was performed to study and visualize the aerodynamic performance of an oblique wing for a high sweep angle. The results obtained were later used to compare with other swept configurations on its stability and control.

Item Type:	Proceeding Paper (Plenary Papers)
Uncontrolled Keywords:	Aerodynamics; Oblique wing; Asymmetric sweep; CFD; Stability
Subjects:	T Technology > TL Motor vehicles. Aeronautics. Astronautics > TL500 Aeronautics
Kulliyyahs/Centres/Divisions/Institutes (Can select more than one option. Press CONTROL button):	Kulliyyah of Engineering > Department of Mechanical Engineering Kulliyyah of Engineering
Depositing User:	Dr Mohamed Ali Jaffar Syed
Date Deposited:	27 Oct 2023 16:24
Last Modified:	27 Oct 2023 16:24
URI:	http://irep.iium.edu.my/id/eprint/107718

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